CN215944904U - Use general quick detach carry structure on unmanned aerial vehicle - Google Patents
Use general quick detach carry structure on unmanned aerial vehicle Download PDFInfo
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- CN215944904U CN215944904U CN202122427265.8U CN202122427265U CN215944904U CN 215944904 U CN215944904 U CN 215944904U CN 202122427265 U CN202122427265 U CN 202122427265U CN 215944904 U CN215944904 U CN 215944904U
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Abstract
The utility model provides a universal quick-release mounting structure applied to an unmanned aerial vehicle, which relates to the technical field of unmanned aerial vehicles and comprises an unmanned aerial vehicle body, wherein the bottom of the unmanned aerial vehicle body is fixedly connected with a frame body, the inner surface of the frame body is provided with a sliding groove, the inner surface of the sliding groove is connected with a loading structure in a sliding way, the loading structure comprises a sliding plate which is connected with the inner surface of the sliding groove in a sliding way, and the bottom surface of the sliding plate is fixedly connected with a loading plate. Magnetic attraction is performed to drive the loading plate to be effectively fixed.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to a universal quick-release mounting structure applied to an unmanned aerial vehicle.
Background
Unmanned aircraft, called "unmanned aerial vehicle" for short, is an unmanned aircraft operated by radio remote control equipment and a self-contained program control device, or is completely or intermittently autonomously operated by an on-board computer, compared with a manned aircraft, the unmanned aerial vehicle is more suitable for tasks which are too dangerous, the unmanned aerial vehicle can be divided into military and civil according to the application field, the unmanned aerial vehicle is divided into a reconnaissance plane and a target plane, and the unmanned aerial vehicle + industrial application is a real and just-needed unmanned aerial vehicle in the civil aspect; the method is currently applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like.
However, in the prior art, current unmanned aerial vehicle is when using, if need carry equipment or carry article, not have fine carry mode, if carry article by force, probably in the flight on the way, because of the carry mode is stable enough and falls down, and in case take place to fall down, article then can produce the damage to cause economic loss.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the defects in the prior art, and the loading structure is used for solving the requirement of articles to be loaded as much as possible, so that the problem that the articles fall off due to the fact that no good loading mode exists is solved.
In order to achieve the purpose, the utility model adopts the following technical scheme: the utility model provides an use general quick detach carry structure on unmanned aerial vehicle, includes the unmanned aerial vehicle body, the bottom fixedly connected with support body of unmanned aerial vehicle body, the spout has been seted up to the internal surface of support body, the internal surface sliding connection of spout has a loading structure, the loading structure include with spout internal surface sliding connection's slide, the bottom surface fixedly connected with load board of slide, load board keeps away from one side surface of slide and has seted up the standing groove, the internal surface of standing groove is provided with first magnet.
As a preferred embodiment, the inner surface of the loading plate is provided with a groove, the outer surface of the frame body is fixedly connected with a fixing plate, the outer surface of the fixing plate is provided with a groove, and the inner surface of the groove is provided with a second magnet.
In a preferred embodiment, the second magnet and the first magnet are opposite to each other in terms of opposite magnetic poles, and a fixing structure is fixedly mounted on an inner surface of the chute.
As a preferred embodiment, the fixing structure includes an adapter plate slidably connected to the sliding plate, a receiving plate is fixedly connected to an outer surface of the adapter plate on a side away from the sliding plate, a return spring is fixedly connected to an outer surface of the receiving plate on a side away from the adapter plate, and a hollow shell is fixedly connected to an end of the return spring away from the receiving plate.
In a preferred embodiment, the inner surface of the hollow shell is provided with a rectangular through hole, and the inner surface of the rectangular through hole is in sliding connection with the outer surface of the bearing plate.
In a preferred embodiment, the rectangular through hole of the hollow shell is fixedly provided with an engaging block, and the outer surface of the engaging block is attached to two sides of the outer surface of the bearing plate.
Compared with the prior art, the utility model has the advantages and positive effects that,
1. when the loading structure needs to be installed, the sliding plate is firstly aligned to the inner surface of the sliding groove, then the sliding plate is slowly pushed into the inner surface of the sliding groove, the sliding plate exerts force on two sides in the sliding process, when the sliding plate moves to the position of the adapting plate, the adapting plate is stressed inwards to exert force to drive the bearing plate to be pressed, the bearing plate drives the return spring to be compressed, then the return spring is compressed, the outward exerting force to drive the adapting plate to clamp and fix the sliding plate, and after the fixing is finished, the first magnet and the second magnet are opposite in different magnetic poles, magnetic adsorption is carried out, so that the loading plate is driven to be effectively fixed.
2. When the loading plate needs to be quickly disassembled, the sliding plate is pulled firstly, then the sliding plate slides on the inner surface of the sliding groove, when the sliding plate slides to the outer surface of the adapting plate, the adapting plate drives the bearing plate to displace, the bearing plate drives the return spring to compress, at the moment, the sliding plate is pulled out, after the sliding plate is pulled out, the first magnet is overturned, after the overturning is finished, the first magnet and the second magnet are opposite to each other in the same magnetic pole, the same magnetic poles repel each other and are gradually far away, and at the moment, the disassembling of the loading plate is finished.
Drawings
Fig. 1 is a front perspective view of a general quick release mounting structure applied to an unmanned aerial vehicle according to the present invention;
fig. 2 is a cross-sectional view of a frame body part of a universal quick release mounting structure applied to an unmanned aerial vehicle according to the present invention;
fig. 3 is a perspective cross-sectional view of a fixing structure of a universal quick release mounting structure applied to an unmanned aerial vehicle according to the present invention.
Illustration of the drawings:
1. an unmanned aerial vehicle body; 2. a frame body; 3. a loading structure; 301. a slide plate; 302. a loading plate; 303. a placement groove; 304. a first magnet; 4. a chute; 5. a fixed structure; 501. a hollow shell; 502. a return spring; 503. a bearing plate; 504. a clamping block; 505. an adapter plate; 6. a fixing plate; 7. a second magnet.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Example 1
As shown in fig. 1-3, the present invention provides a technical solution: the utility model provides an use general quick detach carry structure on unmanned aerial vehicle, including unmanned aerial vehicle body 1, unmanned aerial vehicle body 1's bottom fixedly connected with support body 2, spout 4 has been seted up to the internal surface of support body 2, spout 4's internal surface sliding connection has loading structure 3, loading structure 3 includes slide 301 with 4 internal surface sliding connection of spout, slide 301's bottom surface fixedly connected with loads board 302, load board 302 keeps away from one side surface of slide 301 and seted up standing groove 303, the internal surface of standing groove 303 is provided with first magnet 304, the internal surface of loading board 302 is seted up flutedly, the external fixed surface of support body 2 is connected with fixed plate 6, the recess has been seted up to the surface of fixed plate 6, and the internal surface of recess is provided with second magnet 7, second magnet 7 is relative for the different magnetic pole with first magnet 304, the internal surface fixed mounting of spout 4 has fixed knot to construct 5.
In this embodiment, when the loading structure 3 needs to be installed, first, the sliding plate 301 is aligned to the inner surface of the sliding groove 4, then the sliding plate 301 is slowly pushed into the inner surface of the sliding groove 4, the sliding plate 301 exerts force on two sides during sliding, when the sliding plate 301 is displaced to the position of the adapter plate 505, the adapter plate 505 exerts force on the inner side to drive the bearing plate 503 to be pressed, the bearing plate 503 drives the return spring 502 to be compressed, then the return spring 502 is compressed, the outer force is exerted to drive the adapter plate 505 to clamp and fix the sliding plate 301, after fixing is completed, since the first magnet 304 is opposite to the second magnet 7, magnetic adsorption can be performed, and the loading plate 302 is driven to be effectively fixed.
Example 2
As shown in fig. 1 to 3, the fixing structure 5 includes an adapter plate 505 slidably connected to the sliding plate 301, a receiving plate 503 is fixedly connected to an outer surface of the adapter plate 505 at a side away from the sliding plate 301, a return spring 502 is fixedly connected to an outer surface of the receiving plate 503 at a side away from the adapter plate 505, a hollow shell 501 is fixedly connected to an end of the return spring 502 away from the receiving plate 503, a rectangular through hole is formed in an inner surface of the hollow shell 501, the inner surface of the rectangular through hole is slidably connected to an outer surface of the receiving plate 503, an engaging block 504 is fixedly mounted at the rectangular through hole of the hollow shell 501, and an outer surface of the engaging block 504 is attached to two sides of the outer surface of the receiving plate 503.
In this embodiment, when the loading plate 302 needs to be disassembled quickly, the sliding plate 301 is pulled first, then the sliding plate 301 slides on the inner surface of the sliding slot 4, when the sliding plate 301 slides to the outer surface of the adapting plate 505, the adapting plate 505 drives the receiving plate 503 to displace, the receiving plate 503 drives the return spring 502 to compress, at this time, the sliding plate 301 is pulled out, after the sliding plate 301 is pulled out, the first magnet 304 is turned over, after the turning over is completed, the first magnet 304 and the second magnet 7 are opposite to each other in the same magnetic pole, the same magnetic poles repel each other, and the loading plate 302 is gradually separated, at this time, the disassembling of the loading plate 302 is completed.
The working principle of the embodiment is as follows:
as shown in fig. 1-3, an object to be loaded is first placed in a groove of a loading plate 302, then a sliding plate 301 is fixed, the sliding plate 301 is aligned with an inner surface of a sliding slot 4, then the sliding plate 301 is slowly pushed into the inner surface of the sliding slot 4, the sliding plate 301 exerts forces on two sides during sliding, when the sliding plate 301 is displaced to an adapter plate 505, the adapter plate 505 is forced to exert force inwards to drive a bearing plate 503 to be pressed, the bearing plate 503 drives a return spring 502 to be compressed, then the return spring 502 is compressed, the return spring is forced outwards to drive the adapter plate 505 to clamp and fix the sliding plate 301, after fixing is completed, since the first magnet 304 is opposite to the second magnet 7, magnetic adsorption is performed, so as to drive the loading plate 302 to be effectively fixed, at this time, the unmanned aerial vehicle body 1 can be remotely controlled to fly, when the loading plate 302 needs to be quickly disassembled after flying to the corresponding position, at first pulling slide 301, slide 301 takes place to slide at the internal surface of spout 4 afterwards, slide 301 slides to adapter plate 505's external surface, adapter plate 505 then can drive and accept board 503 and take place the displacement, accept board 503 then drives reset spring 502 and take place the compression, pull out slide 301 this moment can, treat slide 301 and pull out the back, first magnet 304 of upset, first magnet 304 is relative for the homopolar with second magnet 7 this moment after the upset finishes, then like poles repel each other, and keep away from gradually, load board 302 then dismantles at this moment and finishes, then can take out the object, this unmanned aerial vehicle is as flight platform, its function performance mainly realizes through the function that its task load corresponds, through having designed quick detach carry structure, can make different loads can both accomplish quick loading quick replacement in unmanned aerial vehicle flight platform below.
The above description is only a preferred embodiment of the present invention, and not intended to limit the present invention in other forms, and any person skilled in the art may apply the above modifications or changes to the equivalent embodiments with equivalent changes, without departing from the technical spirit of the present invention, and any simple modification, equivalent change and change made to the above embodiments according to the technical spirit of the present invention still belong to the protection scope of the technical spirit of the present invention.
Claims (6)
1. The utility model provides an use general quick detach carry structure on unmanned aerial vehicle, includes unmanned aerial vehicle body (1), its characterized in that: bottom fixedly connected with support body (2) of unmanned aerial vehicle body (1), spout (4) have been seted up to the internal surface of support body (2), the internal surface sliding connection of spout (4) has loading structure (3), loading structure (3) include with spout (4) internal surface sliding connection's slide (301), the bottom surface fixedly connected with of slide (301) loads board (302), one side surface that slide (301) were kept away from in loading board (302) has seted up standing groove (303), the internal surface of standing groove (303) is provided with first magnet (304).
2. The utility model provides an use general quick detach mounting structure on unmanned aerial vehicle according to claim 1 which characterized in that: the inner surface of the loading plate (302) is provided with a groove, the outer surface of the frame body (2) is fixedly connected with a fixing plate (6), the outer surface of the fixing plate (6) is provided with a groove, and the inner surface of the groove is provided with a second magnet (7).
3. The utility model provides an use general quick detach mounting structure on unmanned aerial vehicle according to claim 2 which characterized in that: the second magnet (7) is opposite to the first magnet (304) in terms of different magnetic poles, and a fixing structure (5) is fixedly mounted on the inner surface of the sliding groove (4).
4. The utility model provides an use general quick detach mounting structure on unmanned aerial vehicle according to claim 3 which characterized in that: the fixing structure (5) comprises an adapter plate (505) which is in sliding connection with a sliding plate (301), wherein the adapter plate (505) is fixedly connected with a bearing plate (503) on the outer surface of one side, away from the sliding plate (301), of the adapter plate (505), the bearing plate (503) is fixedly connected with a return spring (502) on the outer surface of one side, away from the adapter plate (505), of the return spring (502), and a hollow shell (501) is fixedly connected with one end, away from the bearing plate (503), of the return spring (502).
5. The utility model provides an use general quick detach mounting structure on unmanned aerial vehicle according to claim 4 which characterized in that: the inner surface of the hollow shell (501) is provided with a rectangular through hole, and the inner surface of the rectangular through hole is in sliding connection with the outer surface of the bearing plate (503).
6. The utility model provides an use general quick detach mounting structure on unmanned aerial vehicle according to claim 5 which characterized in that: the rectangular through hole of the hollow shell (501) is fixedly provided with a clamping block (504), and the outer surface of the clamping block (504) is attached to the two sides of the outer surface of the bearing plate (503).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122427265.8U CN215944904U (en) | 2021-10-09 | 2021-10-09 | Use general quick detach carry structure on unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122427265.8U CN215944904U (en) | 2021-10-09 | 2021-10-09 | Use general quick detach carry structure on unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215944904U true CN215944904U (en) | 2022-03-04 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122427265.8U Expired - Fee Related CN215944904U (en) | 2021-10-09 | 2021-10-09 | Use general quick detach carry structure on unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215944904U (en) |
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2021
- 2021-10-09 CN CN202122427265.8U patent/CN215944904U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220824 Address after: 102488 No. 18 Jianshe Road, Kaixuan Street, Liangxiang, Fangshan District, Beijing-D10246 Patentee after: Air future UAV Technology (Beijing) Co.,Ltd. Patentee after: Jiangxi air future technology innovation Co.,Ltd. Patentee after: Yang Yuchuan Address before: 100000 No. 18 Jianshe Road, Kaixuan street, Liangxiang, Fangshan District, Beijing - d10246 Patentee before: Air future UAV Technology (Beijing) Co.,Ltd. |
|
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 102488 No. 18 Jianshe Road, Kaixuan Street, Liangxiang, Fangshan District, Beijing-D10246 Patentee after: Air future UAV Technology (Beijing) Co.,Ltd. Patentee after: Jiangxi Air Future Technology Innovation Group Co.,Ltd. Patentee after: Yang Yuchuan Address before: 102488 No. 18 Jianshe Road, Kaixuan Street, Liangxiang, Fangshan District, Beijing-D10246 Patentee before: Air future UAV Technology (Beijing) Co.,Ltd. Patentee before: Jiangxi air future technology innovation Co.,Ltd. Patentee before: Yang Yuchuan |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220304 |